发明名称 |
EBW TRIGGERING DEVICE FOR SATELLITE LAUNCH VEHICLE |
摘要 |
An EBW(Exploding BridgeWire) triggering device for a satellite launch vehicle is provided to prevent excessive design of a system and reduce the manufacturing cost by charging a triggering capacitor by using constant voltage. An EBW(Exploding BridgeWire) triggering device for a satellite launch vehicle comprises a flyback conversion section(110) including a flyback transformer and a semiconductor switch to convert input DC into AC. A boosting section(120) comprises a plurality of diodes and capacitors to boost the AC converted by the flyback conversion section to DC output voltage. A triggering capacitor section(130) charges the output voltage boosted by the boosting section. A switch section(150) comprises a trigger circuit unit(152) to supply or block the output voltage charged by the triggering capacitor section.
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申请公布号 |
KR100763558(B1) |
申请公布日期 |
2007.10.04 |
申请号 |
KR20060117707 |
申请日期 |
2006.11.27 |
申请人 |
KOREA AEROSPACE RESEARCH INSTITUTE |
发明人 |
MA, KEUN SU;LIM, YOU CHOL;KIM, MYUNG HWAN;LEE, JAE DEUK |
分类号 |
B64G1/40;B64G1/42;F42C11/00 |
主分类号 |
B64G1/40 |
代理机构 |
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